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22 Cards in this Set
- Front
- Back
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Emergency shut down procedures |
Shut down the affected engine in accordance with the engine shutdown procedure once it has been determined that any of the following adverse conditions has occurred engine fire nacelle overheat engine failure oil pressure out of limits unusual vibrations or roughness excessive fluid leak uncontrollable or excessive power and start valve open light |
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Engine shut down procedure |
1. Engine condition lever feather state no 2. Fite handle pull state no 3.agent discharge switch no 1 4 affected wing isolate wing if fire or overheat condition persists wing isolated A engine bleed air switch off B wing isolation valve or bleed air divider so closed 5 agent discharge switch no 2 6 flaps state position 7 landing state position |
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Apu/gtc emergency procedure |
Apu/gtc fire handle pull 2 agent discharge switch no 1 3 apu isolated A apu 1 no 1 and no 2 engine bleed air switch bleed air divider valve sweet off/closed B apu 3 all engine bleed air sus off 4gtc isolated A all engine bleed air switch off 5 agent discharge switch discharge no 2 no 2 |
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Ground evacuation |
1. Parking brake set 2. Both DC bus ties sws tied 3. Tower notify 4. all engine condition levers feather 5 all fire handles pull 6. Notify crew pax using pa action easy Victor 7. Alarm bell on/wait 5 secs off 8. Pax evacuate A before opening exits assess conditions to ensure they are usable B clearly and promptly say unfastened seat belts leave everything behind come this way C direct/assist pax away from a/c D check cargo compartment ensure crew/pax evacuated E administer first aid as required 9. DC power switch off 10. Aircraft chock |
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Directional control problems throttles in ground range |
Throttles ground idle Brakes as req'd Symmetrical engines reverse Engineering shutdown procedure shutdown no |
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Throttles in flight range directional control problems |
Throttles flight idle Brakes as req'd Esp shutdown no Throttles ground idle Symmetrical engines reverse |
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Brake system failure |
Brake select sw emer Aug pump sw on Check aux hydraulic system and emrg brk pressure |
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Anti skid failure |
Anti skid sw off |
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Propeller malfunctions during take off after v1 |
When safely airborne retract landing gear while accelerating to a two eng inop vmca Property gov control sw mech If malfunction is eliminated continue in mech mode If malfunction persists accelerate & maintain as near 150 kias as possible If an immediate landing is feasible engine shutdown procedure |
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Engine failure during takeoff after v1 |
Engine shut down procedure shutdown no as req'do Landing gear up Airspeed/flaps accelerate to three engine climb speeds Retract flaps as Airspeed permits |
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Torching |
Starter sw hold to starter limit Engine condition lever ground stop Starter sw release are starter limit |
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Tailpipe fire |
Tail pipe fire engine shutdown procedure |
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Over temperature |
Throttle affected engine move towards flight idle Td sw null If condition persists engine shutdownprocedure |
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Throttle control failure |
Throttle control failure. release affected throttle in place Engine shutdownprocedure |
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Rapid decompression |
Crew/pax notify O2 mask/oxygen regulator/mic sw. Don/100% oxygen/ mask mic check in Seat belts light sw on Seat belts fastenot Fuselage inspect for damage Descent as req'd |
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Wing fire |
Engine bleed air sws off Affected engine Wings isolation valve closed Bleed air divider sw closed Fuel crossfeed valve sw. Closed/depressurize manifold |
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Fire smoke fume elimination |
Crew/pax notify O2 mask/oxygen regukator/mic sw. Don/ 100% oxygen/ oxygen mask mic/ check in Firefighter mask/oxygen. Don/100% oxygen Seat belt light sw on Seat belts fastenot Smoke goggles as req'd |
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Flight control booster assy failure |
Verify that the controls match the hard over manoeuvre. Failure verified Gaurd ed booster control switch(es) affected control. Off |
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Rudder trim tab system failure |
Air speed reduce until directional control is regained Rudder trim tab sw hold in opposite direction Trim tab rudder c/b 6e2 open |
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Elevator trim tab system failure |
Elevator trim tab sws hold in opposite direction Elev tab power switch off then emer Elevator trim emer sw operate to re trim ac |
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Elevator trim fail annunciation illumination |
Trim fail annunciator illuminated. Anticipate an out of trim condition Ap-ap levery disengaged Elevator trim manual retrimode Back page prepare for a possible out of trim condition Disengage autopilot light extinguisheswitch Manual retrim |
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Asymmetric wing flap condition |
Flapso control lever reset to correspond to position of the flaps Mission consideration no further movement of flaps by any means |
